| Thermal Cracking and Heat Sink Capacity of Aviation Kerosene Under Supercritical Conditions | |
Zhong FQ(仲峰泉) ; Fan XJ(范学军); Yu G(俞刚); Li JG(李建国); Sung CJ; Zhong, FQ (reprint author), Chinese Acad Sci, Inst Mech, Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China
| |
| Source Publication | Journal of Thermophysics and Heat Transfer
 |
| 2011 | |
| Volume | 25Issue:3Pages:450-456 |
| ISSN | 0887-8722 |
| Abstract | Thermal cracking and endothermicity of China No. 3 aviation kerosene were studied experimentally under supercritical conditions relevant to regenerative cooling systems for scramjet applications. A multiple-stage heating system with reaction products collection was used that can achieve a fuel temperature range of 780-1050 K, a pressure range of 3-4.5 MPa, and a residence time range of 0.6-3 s. The chemical heat sink was determined through a control volume analysis of the fuel flow. Compositions of I he cracked gaseous and liquid products were analyzed via gas chromatography. Based on the results of fuel conversion, the temperature range for the active cracking was observed to be approximately 800-1000 K, beyond which the cracking approaches completion. It was also found that the variation of the chemical heat sink with temperature can be nonmonotonic and a maximum endothermicity was seen to occur in the temperature range of 900-960 K, depending on the residence time. For the current operation conditions, the maximum chemical heat sink reached 0.5 MJ/k g at a fuel conversion of 45%. Composition analysis of the gaseous product indicated that the saturated hydrocarbons such as methane became dominant as temperature was increased. On the other hand, the major compositions of the liquid product were benzene-based and naphthalene-based hydrocarbons. |
| Keyword | Tetralin Decalin |
| Subject Area | Thermodynamics ; Engineering |
| DOI | 10.2514/1.51399 |
| URL | 查看原文 |
| Indexed By | SCI ; EI |
| Language | 英语 |
| WOS ID | WOS:000293259600015 |
| WOS Keyword | TETRALIN ; DECALIN |
| WOS Research Area | Thermodynamics ; Engineering |
| WOS Subject | Thermodynamics ; Engineering, Mechanical |
| Department | LHD高超声速推进技术 |
| Classification | Q3 |
| Citation statistics | |
| Document Type | 期刊论文 |
| Identifier | http://dspace.imech.ac.cn/handle/311007/45173 |
| Collection | 高温气体动力学国家重点实验室 |
| Corresponding Author | Zhong, FQ (reprint author), Chinese Acad Sci, Inst Mech, Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China |
| Recommended Citation GB/T 7714 | Zhong FQ,Fan XJ,Yu G,et al. Thermal Cracking and Heat Sink Capacity of Aviation Kerosene Under Supercritical Conditions[J]. Journal of Thermophysics and Heat Transfer,2011,25,3,:450-456. |
| APA | 仲峰泉,范学军,俞刚,李建国,Sung CJ,&Zhong, FQ .(2011).Thermal Cracking and Heat Sink Capacity of Aviation Kerosene Under Supercritical Conditions.Journal of Thermophysics and Heat Transfer,25(3),450-456. |
| MLA | 仲峰泉,et al."Thermal Cracking and Heat Sink Capacity of Aviation Kerosene Under Supercritical Conditions".Journal of Thermophysics and Heat Transfer 25.3(2011):450-456. |
| Files in This Item: | Download All | |||||
| File Name/Size | DocType | Version | Access | License | ||
| SCI-J2011098.pdf（57KB） | 开放获取 | -- | View Download | |||
Items in the repository are protected by copyright, with all rights reserved, unless otherwise indicated.
Edit Comment